lighter-than-air vehicles - Defense Innovation Marketplace

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Appendix C – AbbreviationsProgramsATBHALE-DISISJLENSLEMVPGSSPTDSRAIDREAPSTMPASTARSAerostat Test BedHigh-Altitude Long Endurance DemonstratorIntegrated Sensor is StructureJoint Land Attack Cruise Missile Defense Elevated Netted SensorSystemLong Endurance Multi-Intelligence VehiclePersistent Ground Surveillance SystemPersistent Threat Detection SystemRapid Aerostat Initial DeploymentRapidly Elevated Aerostat PlatformsSmall, Tactical, Multi-Payload Aerostat SystemTethered Aerostat Radar SystemTermsAA2QAAEABOAEWEAFBAFRLAFWAAGLAMUSAQIARARGUSARLAROCARSTRATASA(ALT)ASD(R&E)Air Force ISR Innovations DivisionArmy Acquisition ExecutiveArmy Budget OfficeArmy Expeditionary Warrior ExperimentAir Force BaseAir Force Research LaboratoryAir Force Weather AgencyAbove Ground LevelAerostat Mounted UTAMSAcquisitions DivisionArmy RequirementsAutonomous Real-time Ground Ubiquitous Surveillance ImagingSystemArmy Research LaboratoryArmy Requirements Oversight CouncilArmy Forces STRATegic CommandAssistant Secretary of the Army for Acquisition, Logistics, andTechnologyAssistant to the Secretary of Defense (Research and Engineering)C-1
ATECAVAWSSBBAAVBCTBLOSCC2C3IC4ISRC5ISRCD/CNTCDDCDLsCDRTCENTCOMC-IEDCLRCOCOMCOMMSCONUSCOPCOSHCPDDDARPADoDDHSDMTIDTEEMDEO/IREPGArmy Test and Evaluation CommandAir VehicleAirborne Weapons Surveillance SystemBuoyancy Assisted Lift Air VehicleBattle Command TeamBeyond Line of SightCommand and ControlCommand, Control, Communications and IntelligenceCommand, Control, Communications, Computers ISRCommand, Control, Communications, Computers, Combat Systems,Intelligence, Surveillance, and ReconnaissanceCounterdrug/Counter-NarcoterrorismCapabilities Definition DocumentCommon Data LinksCapability Development for Rapid TransitionCentral CommandCounter-Improvised Explosive DeviceCapabilities and Limitations ReportCombatant CommandCommunicationsContinental United StatesCommand Observation PostControl of Static HeavinessCapability Production DocumentDefense Advanced Research Projects AgencyDoD Department of DefenseDepartment of Homeland SecurityDismount Moving Target IndicatorDevelopmental TestingEngineering and Manufacturing DevelopmentElectro-optical/InfraredElectronic Proving GroundC-2
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SUMMARY REPORT OF DoD FUNDED LIGHTE
Page 3 and 4:
TABLE OF CONTENTSEXECUTIVE SUMMARY
Page 5 and 6:
Figure 11: Computer Rendering of Al
Page 7 and 8:
Table 22: HALE-D Program Overview .
Page 9 and 10:
EXECUTIVE SUMMARYIn the Senate repo
Page 11 and 12:
for unmanned aerial vehicle and cru
Page 13 and 14:
Integrated Sensor Is Structure (ISI
Page 15 and 16:
PREFACECongress, through the Senate
Page 17 and 18:
PURPOSEThe purpose of this document
Page 19 and 20:
INTRODUCTIONBackgroundModern LTA cr
Page 21 and 22:
ground, large aerostats are anchore
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AirliftAirships, particularly hybri
Page 25 and 26:
AEROSTAT PROGRAMSAerostats are air
Page 27 and 28:
Aerostat Test Bed (ATB)Table 2: ATB
Page 29 and 30: AltusTable 4: Altus Program Overvie
Page 31 and 32: would otherwise lack organic survei
Page 33 and 34: Table 7: JLENS Technical Specificat
Page 35 and 36: Persistent Ground Surveillance Syst
Page 37 and 38: and advance systems capabilities as
Page 39 and 40: Length: 117 ft.Width: 39 ft.Height:
Page 41 and 42: Rapid Aerostat Initial Deployment (
Page 43 and 44: Rapidly Elevated Aerostat Platforms
Page 45 and 46: tether lengths to support different
Page 47 and 48: Length: 26.87 ft.Table 17: STMPAS T
Page 49 and 50: Table 19: TARS Technical Specificat
Page 51 and 52: AIRSHIP PROGRAMSDespite the fact th
Page 53 and 54: Figure 30: Size Comparison for Hybr
Page 55 and 56: Table 21: Blue Devil 2 Technical Sp
Page 57 and 58: High-Altitude Long Endurance-Demons
Page 59 and 60: HiSentinelTable 24: HiSentinel Prog
Page 61 and 62: Table 26: Comparison of HiSentinel
Page 63 and 64: Table 28: ISIS Technical Specificat
Page 65 and 66: Table 30: LEMV Technical Specificat
Page 67 and 68: MZ-3AVehicle Class: Conventional Ai
Page 69 and 70: PelicanTable 33: Pelican Program Ov
Page 71 and 72: Figure 53: Illustration Showing Lig
Page 73 and 74: Table 36: Skybus Technical Specific
Page 75 and 76: APPENDICESAppendix A- BalloonsIntro
Page 77 and 78: could be separated from the balloon
Page 79: Appendix B - Glossary of TermsAAero
Page 83 and 84: IFFIPTISRITSJJCTDJIEDDOJMUAJROCJUON
Page 85 and 86: SIGINTSINCGARSSIPRNetSMDBLSMDCSRVSu
Page 87 and 88: Appendix D - References1. The Senat
Page 89 and 90: 43. “Lockheed Martin ISIS”. HIS
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